#Bombardier challenger 300 x plane pro
The avionics suite is based on a Rockwell Collins Pro Line 21 with four 10in x 12in liquid crystal displays, an integrated four-tube electronic flight instrumentation system (EFIS) and a two-tube engine in-flight condition monitoring system (EIFCMS). The ergonomically designed flight deck accommodates two crew. The high cruise speed is Mach 0.82 or 870km/h and the maximum operating altitude is 45,000ft or 13,716m. The main performance parameters are the aircraft’s non-stop range of 5,741km combined with its ability to take-off from airstrips of 1,509m. The component sections are transported to the Bombardier Aerospace Montreal Dorval facility for final assembly. Hawker De Havilland Australia supplies the tailcone and the auxiliary power installation unit. The rear fuselage and tail are built by AIDC of Taiwan. Canadair is responsible for building the forward section of the fuselage including the cockpit and primary flight controls.Mitsubishi Heavy Industries builds the wings.īombardier Aerospace in Belfast is responsible for construction of the centre fuselage. The Challenger 300 has a conventional all-metal airframe. With two pilots and eight passengers, the Challenger 300 travelled the 4,365km (2,712 miles) in 4 hours 41 minutes, cruising at an average speed of 921km/h (572mph). In November 2004, the aircraft set a world speed record for its class for a journey from Carlsbad, California, to Bangor, Maine. Deliveries are scheduled to begin in late 2008. In September 2007, XOJET of San Carlos, California, placed the largest single order received for the Challenger 300 – a firm order for 20 jets with options for an additional 60 aircraft. All aircraft operations are professionally managed on the owners’ behalf by Flexjet, including flight crew employment and maintenance for a fixed monthly management fee. The 200th Challenger 300 jet was delivered in August 2008 to Vistajet.īombadier has received firm orders for over 220 aircraft, including 17 for Bombardier’s subsidiary company Flexjet based in Dallas and Flexjet Europe in Hounslow, UK, for its fractional ownership programme.īy owning a fractional interest in the aircraft, corporate customers have the availability of business jet travel. The Challenger 300 entered service with Flexjet in January 2004. The aircraft received certification from Transport Canada in May 2003, US Federal Aviation Authority in June 2003 and European Joint Aviation Authorities in August 2003. The aircraft was launched in 1999 and the first flight of the aircraft took place in August 2001 from Bombardier’s Learjet plant in Wichita, Kansas. "The Challenger 300 carries up to eight passengers over a non-stop range of 3,100nm." coast-to-coast range across America, using a take-off airfield length of less than 5,000ft. The aircraft carries up to eight passengers in a cabin with stand-up headroom over a non-stop range of 3,100nm, i.e. The aircraft was renamed in September 2002. The Challenger 300, originally known as the Continental Business Jet BD-100, is medium size trans-continental business jet from Bombardier Aerospace of Canada. The Challenger 300 requires a take-off airfield length of less than 5,000ft.
The aircraft has two Honeywell AS907 turbofan engines each providing 35.81kN (8,050lbs) thrust. The aircraft can carry up to eight passengers coast-to-coast across America.īombadier's comprehensive flight test programme involved five aircraft. Rockwell Collins was given the task of supplying the Pro Line 21 integrated avionics system. The Bombardier Challenger 300 flight deck. The third Bombardier Challenger 300 business jet successfully completed its first flight on 6 December 2001, shown here taking off from Wichita's Mid-Continent airport. Interior of Bombardier's Challenger 300 business jet for executive and corporate business travel. The Bombardier Challenger 300 (formerly called the Continental) business jet entered service with Flexjet in January 2004.